View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00020U 26128.80895659 +.00000000 +00000-0 +14968-3 0 00005
2 00020 33.3491 48.7026 1637703 202.5047 149.4829 11.61944420 00
| Epoch (UTC): | 08 May 2026 19:24:53 |
| Eccentricity: | 0.1637703 |
| inclination: | 33.3491° |
| perigee height: | 507 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 48.7026° |
| argument of perigee: | 202.5047° |
| revolutions per day: | 11.61944420 |
| mean anomaly at epoch: | 149.4829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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